发明名称 |
ACTIVE SYNCHRONIZING RING |
摘要 |
An improved system, apparatus and method for controlling vane angles in a gas turbine engine, and more specifically, for correcting vane angle error in a gas turbine engine. An active synchronization ring comprises a plurality of micro-actuators coupled to the synchronization ring to correct distortion in the synchronization ring. The micro-actuators apply a bending moment to the synchronization ring to cancel or compensate for synchronization ring distortion. The micro-actuators may be controlled open loop or closed loop. Strain sensors measure ring distortion and provide signals to the controller for closed loop control. |
申请公布号 |
US2015184535(A1) |
申请公布日期 |
2015.07.02 |
申请号 |
US201414576858 |
申请日期 |
2014.12.19 |
申请人 |
Rolls-Royce North American Technologies, Inc. |
发明人 |
Dougherty Michael P. |
分类号 |
F01D17/16;F01D9/04 |
主分类号 |
F01D17/16 |
代理机构 |
|
代理人 |
|
主权项 |
1. A system for controlling individual vane angles in a gas turbine engine, comprising:
a synchronization ring having a plurality of micro-actuators coupled to said synchronization ring, each of said micro-actuators create a bending moment in said synchronization ring, each of said micro-actuators having an input for receiving a control signal; and an actuator pivotally attached to said synchronization ring for rotating said ring about an axis. |
地址 |
Indianapolis IN US |